View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65547U 26088.12904637 +.00000000 +00000-0 +11117-3 0 00000
2 65547 85.9859 79.2659 0002460 69.8301 290.3146 14.12431248 05
| Epoch (UTC): | 29 March 2026 03:05:49 |
| Eccentricity: | 0.0002460 |
| inclination: | 85.9859° |
| perigee height: | 849 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 79.2659° |
| argument of perigee: | 69.8301° |
| revolutions per day: | 14.12431248 |
| mean anomaly at epoch: | 290.3146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|